CN201702910U - Injection molding machine template - Google Patents

Injection molding machine template Download PDF

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Publication number
CN201702910U
CN201702910U CN2010202266011U CN201020226601U CN201702910U CN 201702910 U CN201702910 U CN 201702910U CN 2010202266011 U CN2010202266011 U CN 2010202266011U CN 201020226601 U CN201020226601 U CN 201020226601U CN 201702910 U CN201702910 U CN 201702910U
Authority
CN
China
Prior art keywords
template
code mask
free bearing
hinge seat
mold
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN2010202266011U
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Chinese (zh)
Inventor
刘伟波
阮长柏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
GUANGZHOU HUAYAN PRECISION MACHINERY CO Ltd
Original Assignee
GUANGZHOU HUAYAN PRECISION MACHINERY CO Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by GUANGZHOU HUAYAN PRECISION MACHINERY CO Ltd filed Critical GUANGZHOU HUAYAN PRECISION MACHINERY CO Ltd
Priority to CN2010202266011U priority Critical patent/CN201702910U/en
Application granted granted Critical
Publication of CN201702910U publication Critical patent/CN201702910U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to an injection molding machine template which at least comprises a stacking template used for installing a mold, an upper hinge seat and a lower hinge seat which are arranged on the back surface of the stacking template, and guide seats which hare distributed at the four corners of the stacking template. A flange which protrudes the surface of the back surface of the stacking template is arranged on the periphery of the back surface of the stacking template. Continuous and closed back ribs are arranged on the back surface of the stacking template. The guide seats are connected on the back ribs. An inclined rib which forms an angle with the stacking template is connected among the upper hinge seat, the lower hinge seat and the stacking template. A back plate is connected between the upper hinge seat and the lower hinge seat. The transverse stressed area of the template is concentrated at the central part of the template, the longitudinal mold clamping force is transferred to the central part of the mold through the upper hinge seat and the lower hinge seat, the stress state of the template and the mold is greatly improved, the bending deformation of the template and the mold is reduced or avoided, the service life of the template and the mold is improved, the qualification rate of the products is improved, the motion controllability of the template is improved and the realization of the high-precision mold protection is facilitated; and the template is ensured to have enough rigidity and the amount of the used materials is relative small.

Description

The Jet forming machine template
Technical field
The utility model relates to a kind of accessory of Jet forming machine, is specifically related to a kind of Jet forming machine template.
Background technology
In the industrial production, adopt the technology of ejection formation to make plastic products mostly with definite shape.
In the existing ejection formation machinery, all be to provide mold clamping force and ejecting force for mould by clamping.Existing mechanical reaming type matched moulds system, mainly by solid plate, moving platen, tailgate, machine hinge and guide pillar constitute, and template is as the important stressed part in the clamping, and the deflection when it is stressed directly influences the quality and the die life of plastic products.
At present, in mechanical reaming type matched moulds system, moving platen is designed to be made into horizontal " U " shape structure that is shown in Fig. 1 a, 1b usually, to satisfy mechanism's assembling and force request, its stressing conditions as shown in Figure 2, the clamp force that machine hinge R1, R2 transmit finally roughly acts on both mold ends, mould is more little or mold stiffness is poor more, template deformation amount δ is big more, causes the possibility of plate bursting or goods overlap also big more.The shortcoming of this type structure is finally to act on template and both mold ends portion by the mold clamping force that the machine hinge is delivered on the mould, cause the stressed back of template and mould to produce bigger flexural deformation, thereby make plastic products the defective of overlap occur, simultaneously template and die life have also been produced considerable influence; When using the relatively poor mould (as the PET preform mould) of rigidity, above-mentioned defective is particularly outstanding, even can't guarantee that goods are qualified, has a strong impact on die life, has reduced product qualified rate, and has increased production cost.
In sum, develop a kind of stressed rational Jet forming machine template, become the focus of paying close attention in the industry.
The utility model content
At the deficiencies in the prior art, the purpose of this utility model is intended to provide a kind of Jet forming machine template, and it is stressed rationally, when having guaranteed that goods have higher qualification rate, also possesses long service life.
For achieving the above object, the utility model adopts following technical scheme:
A kind of Jet forming machine template, at least comprise the code mask of installing for mould, be positioned at the last free bearing and the following free bearing at the described code mask back side, and the guide holder of distribution and described code mask quadripolar corners, the described code mask back side is provided with and protrudes from its surperficial flange, described code mask back side periphery is provided with continuously and the back of the body rib of sealing, and described guide holder is connected on the described back of the body rib; Describedly go up free bearing, also be connected with one between free bearing and the code mask down and have the diagonal rib of angle with code mask; Described going up between free bearing and the following free bearing also is connected with a backboard.
The two ends of described backboard are connected with the top ends of described diagonal rib.
Described code mask, diagonal rib, last free bearing, following free bearing, backboard longitudinally are being shaped to a trapezoidal shape that seals perpendicular to the projection on the face of described code mask.
The angle of described diagonal rib and described code mask is 45 °.
Described diagonal rib is positioned at the middle part of described code mask width in the projection at the code mask back side; Described diagonal rib is connected in the middle part of described code mask short transverse.
Described diagonal rib and described free bearing and/or the free bearing structure that is formed in one down of going up.
The Jet forming machine template that the utility model is set forth, its beneficial effect is:
In the lateral stressed set of regions of template in the middle, and make vertical mold clamping force be delivered to the mould middle part by upper and lower free bearing, greatly improved the force-bearing situation of template and mould, reduce or avoid the flexural deformation of template and mould, improve the service life of template and mould, improve the qualification rate of goods, improve the motion controllability of template, be beneficial to and realize high-precision mould protection; Simultaneously, guarantee that template has enough rigidity, and less relatively with material.
Description of drawings
Fig. 1 a is a kind of Jet forming machine formwork structure of prior art schematic diagram;
Fig. 1 b is the D-D cutaway view of Fig. 1 a;
Fig. 2 is the stressing conditions schematic diagram of the Jet forming machine template shown in Fig. 1 a;
Fig. 3 is the structural representation of a kind of Jet forming machine template of the utility model;
Fig. 4 is that the A of Fig. 3 is to view;
Fig. 5 is the rearview of Fig. 4;
Fig. 6 is the B-B cutaway view of Fig. 4;
Fig. 7 is the C-C cutaway view of Fig. 5;
Fig. 8 is the user mode schematic diagram of Jet forming machine template shown in Figure 3.
The specific embodiment
Below, in conjunction with the accompanying drawings and the specific embodiment, Jet forming machine template of the present utility model is described further, so that clearerly understand the utility model technological thought required for protection.
Shown in Fig. 3,4,5,6,7, (X is to the width of describing the Jet forming machine template in the diagram for a kind of Jet forming machine template of the present utility model, Z is to describing its short transverse), main body is rectangular structure, it comprises code mask 1, code mask is provided with a plurality of installing holes, for the installation connection of mould; Have the flange 8 that is provided with continuously along its periphery on code mask 1, the last end face of flange 8 protrudes from code mask 1 back surfaces, thus, has increased the edge thickness of code mask 1, has strengthened its flexing resistance.
Be provided with back of the body rib 6 at code mask 1 back side, its back at code mask 1 is provided with and surrounds an enclosed construction continuously; Back of the body rib 6 is positioned at the centre position of code mask 1 along height, width, and the installing hole that connects for mould on the code mask 1 all is positioned at the enclosed construction that back of the body rib 6 surrounds, and during duty, back of the body rib 6 directly bears the active force of mould to code mask 1.
At code mask 1 back side, also be provided with free bearing 3, following free bearing 4, its two be installed on the middle part of code mask 1 width, between the top of the two, be provided with backboard 5 at it with its two connection.Between last free bearing 3 and the code mask 1, down all be connected with diagonal rib 2 between free bearing 4 and the code mask 1, diagonal rib 2 is positioned at the centre position of code mask 1 width, and, correspondence goes up two diagonal ribs, the 2 mutual symmetries of free bearing 3 and following free bearing 4 respectively, and the tie point of two diagonal ribs 2 and code mask 1 is near the centre position of code mask 1 short transverse.Thereby referring to shown in Figure 6, the longitudinal profile of code mask 1, two diagonal ribs 2, last free bearing 3, following free bearing 4 and backboard 5 is shaped to an enclosed construction that class is trapezoidal.
In order to increase the intensity of said structure, last free bearing 3, following free bearing 4, the integrated formed structure of diagonal rib 2 for adopting casting technique to be made.
Four vertex angle parts at back of the body rib 6 also are connected with guide holder 7, and it is provided with the pilot hole perpendicular to code mask 1 back side, and, be provided with breach with guide holder 7 couplings at four vertex angle parts of code mask 1.
As shown in Figure 8, when above-mentioned Jet forming machine template is used, mould E is installed in the front surface of code mask, the machine hinge is delivered to the clamp force F of free bearing 3 and following free bearing 4 along the direction as shown transmission, finally affact the position of mould E by pars intermedia, make the active force can not put on the edge of mould, reduced the arm of force that mould is subjected to active force, effectively improved the force-bearing situation of mould.
Again as shown in Figure 6, above-mentioned diagonal rib 2 is set to 45 ° with the angle a of code mask 1, and to realize better force transmission effect, certainly, connection angle, position, the quantity of diagonal rib 2 on code mask 1 all can be made corresponding design as required.
Relative common templates, the utility model has greatly improved the force-bearing situation of template and mould, effectively reduces or avoid the flexural deformation of template and mould, improves the service life of template and mould, avoids the template excessive deformation to cause plate bursting or product defect.Under the prerequisite that guarantees formwork rigidity, the utility model has improved stock utilization, reduces the use of material, and the motion controllability of template is improved, and can realize high-precision mould protection.
For a person skilled in the art, can make other various corresponding changes and distortion, and these all changes and distortion should belong within the protection domain of the utility model claim all according to technical scheme described above and design.

Claims (6)

1. Jet forming machine template, at least comprise the code mask of installing for mould, be positioned at the last free bearing and the following free bearing at the described code mask back side, and the guide holder of distribution and described code mask quadripolar corners, it is characterized in that, described code mask back side periphery is provided with and protrudes from its surperficial flange, and the described code mask back side is provided with continuously and the back of the body rib of sealing, and described guide holder is connected on the described back of the body rib; Describedly go up free bearing, also be connected with one between free bearing and the code mask down and have the diagonal rib of angle with code mask; Described going up between free bearing and the following free bearing also is connected with a backboard.
2. Jet forming machine template as claimed in claim 1 is characterized in that, the two ends of described backboard are connected with the top ends of described diagonal rib.
3. Jet forming machine template as claimed in claim 2 is characterized in that, described code mask, diagonal rib, last free bearing, following free bearing, backboard longitudinally are being shaped to a trapezoidal shape that seals perpendicular to the projection on the face of described code mask.
4. Jet forming machine template as claimed in claim 1 is characterized in that, the angle of described diagonal rib and described code mask is 45 °.
5. Jet forming machine template as claimed in claim 1 is characterized in that, described diagonal rib is positioned at the middle part of described code mask width in the projection at the code mask back side; Described diagonal rib is connected in the middle part of described code mask short transverse.
6. Jet forming machine template as claimed in claim 1 is characterized in that, described diagonal rib and described free bearing and/or the free bearing structure that is formed in one down of going up.
CN2010202266011U 2010-06-12 2010-06-12 Injection molding machine template Expired - Fee Related CN201702910U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010202266011U CN201702910U (en) 2010-06-12 2010-06-12 Injection molding machine template

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010202266011U CN201702910U (en) 2010-06-12 2010-06-12 Injection molding machine template

Publications (1)

Publication Number Publication Date
CN201702910U true CN201702910U (en) 2011-01-12

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CN2010202266011U Expired - Fee Related CN201702910U (en) 2010-06-12 2010-06-12 Injection molding machine template

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102001165A (en) * 2010-06-12 2011-04-06 广州华研精密机械有限公司 Template of injection molding machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102001165A (en) * 2010-06-12 2011-04-06 广州华研精密机械有限公司 Template of injection molding machine
CN102001165B (en) * 2010-06-12 2014-07-23 广州华研精密机械有限公司 Template of injection molding machine

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP02 Change in the address of a patent holder

Address after: 511340, No. 6, founding Road, Xintang Town, Guangzhou, Guangdong, Zengcheng

Patentee after: Guangzhou Huayan Precision Machinery Co., Ltd.

Address before: 510315, No. 718, Pioneer Road, Guangzhou, Guangdong, Luogang District

Patentee before: Guangzhou Huayan Precision Machinery Co., Ltd.

C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110112

Termination date: 20140612